Flash Suppressor for Firearm

ABSTRACT

Novel flash suppressors comprised of tines formed by cuts of varied lengths and widths to better reduce muzzle flash and eliminate any unwanted ringing caused by resonance of the tines.

RELATED APPLICATIONS

This application is a divisional of U.S. patent application Ser. No.14/465,060, filed Aug. 21, 2014 by Kurtis A. Palu and titled, “FlashSuppressor for Firearm” (attorney docket no. 0641.03), which isincorporated herein by reference in its entirety.

COPYRIGHT STATEMENT

A portion of the disclosure of this patent document contains materialthat is subject to copyright protection. The copyright owner has noobjection to the facsimile reproduction by anyone of the patent documentor the patent disclosure as it appears in the Patent and TrademarkOffice patent file or records, but otherwise reserves all copyrightrights whatsoever.

FIELD

The present disclosure relates, in general, to a flash suppressor for afirearm, and more particularly, to a flash suppressor that includes aplurality of tines formed in a way to better reduce muzzle flash andeliminate any unwanted ringing caused by resonance of the tines.

BACKGROUND

In order to fire a projectile, a firearm utilizes an ignited propellantto create a high-pressure pulse of hot gases behind the projectile toforce the projectile down the barrel of the firearm. When a projectileis fired from most firearms, a visible signature or flash, commonlyreferred to as “muzzle flash,” exits the barrel of the firearm after thedischarge of the projectile. Muzzle flash has a number of undesirableeffects, including temporarily impairing the vision of the person usingthe firearm, particularly in cases where the person is using the firearmin limited light conditions. Muzzle flash is caused by a number offactors, including propellant gases exiting the barrel of the firearmafter the projectile and the mixture of such gases with the ambient air.The severity of muzzle flash depends on number of factors, including thetype of firearm and ammunition being used. Muzzle flash is often moresevere in firearms with shorter barrels because there is less distancefor the propellant to be consumed before exiting the barrel.

Muzzle flash can be reduced through the use of a flash hider, whichattaches to end of the firearm barrel and mechanically disperses thegases exiting the firearm in a way to reduce the visible flash. Flashhiders come is variety of designs, including the use of a plurality ofprongs, or tines, extending from the end of the barrel of firearm.However, when flash hiders use tines to reduce muzzle flash, thehigh-pressure gases exiting the firearm can cause the tines to resonateand cause an undesirable ringing sound. In addition, tines used incertain flash hiders may be relatively long and vary in length. Tinesthat vary in length can create a number of difficulties, including, forexample, making it difficult to attach other firearm components such asa noise suppressor to the flash suppressor. Having tines of differentlength also can result in the longer tine catching on debris and otherimpediments during field use and absorbing the majority of the impact ifthe firearm receives an impact at its distal end, such as being droppedon its barrel.

Accordingly, there is a need for a flash suppressor that effectivelysuppresses muzzle flash without creating any ringing or otherundesirable sound effects, but which can also be effectively used in afield environment and designed so that other firearm components can beeasily attached to it.

BRIEF SUMMARY

Certain embodiments include flash suppressors for firearms thateffectively suppress muzzle flash using a plurality of tines of equalmass oriented in a helical manner. In certain embodiments, each tineextends to the same plane perpendicular to the distal end of the flashsuppressor and the cuts used to form the tines vary in length and/orwidth in order to prevent an audible ringing or other undesirableeffects. In addition, in certain embodiments, each tine contains agroove in its outer surface where each groove can be varied in length,width and/or depth in order to reduce the weight of the tine and toachieve other desired effects. In aspects of certain embodiments, acircular face of the flash hider located adjacent to the muzzle containsa bore that has the same circumference as the bore formed by theinternal surfaces of the tines.

The embodiments of the invention described herein are defined by theclaims. Further advantages and a more complete understanding of theembodiments will be apparent to persons skilled in the art from reviewfollowing detailed description of various embodiments and appendedclaims.

BRIEF DESCRIPTION OF THE DRAWINGS

A further understanding of the nature and advantages of particularembodiments may be realized by reference to the remaining portions ofthe specification and the drawings, in which like reference numerals areused to refer to similar components.

FIG. 1 shows a side view of an embodiment of the present invention.

FIG. 2 shows a perspective end view of the proximal end of the flashsuppressor of FIG. 1.

FIG. 3 is a perspective view of an individual tine of the flashsuppressor of FIG. 1.

FIG. 4 is an exploded perspective view of the flash suppressor of FIG.1.

FIG. 5 is a view of the distal end of the flash suppressor of FIG. 1.

FIG. 6 is a side view of the flash suppressor of FIG. 1.

FIG. 7 is a side view of the flash suppressor of FIG. 1 from theopposite side shown in FIG. 6.

DETAILED DESCRIPTION OF CERTAIN EMBODIMENTS

While various aspects and features of certain embodiments have beensummarized above, the following detailed description illustrates a fewexemplary embodiments in further detail to enable one of skill in theart to practice such embodiments. The described examples are providedfor illustrative purposes and are not intended to limit the scope of theinvention.

In the following description, for the purposes of explanation, numerousspecific details are set forth in order to provide a thoroughunderstanding of the described embodiments. It will be apparent to oneskilled in the art, however, that other embodiments of the presentinventions may be practiced without some of these specific details.Several embodiments are described herein, and while various features areascribed to different embodiments, it should be appreciated that thefeatures described with respect to one embodiment may be incorporatedwith other embodiments as well. By the same token, however, no singlefeature or features of any described embodiment should be consideredessential to every embodiment of the invention, as other embodiments ofthe invention may omit such features.

Unless otherwise indicated, all numbers used herein to expressquantities, dimensions, and so forth should be understood as beingmodified in all instances by the term “about.” In this application, theuse of the singular includes the plural unless specifically statedotherwise, and use of the terms “and” and “or” means “and/or” unlessotherwise indicated. Moreover, the use of the term “including,” as wellas other forms, such as “includes” and “included,” should be considerednon-exclusive. Also, terms such as “element” or “component” encompassboth elements and components comprising one unit and elements andcomponents that comprise more than one unit, unless specifically statedotherwise.

FIG. 1 is a side view of an exemplary flash suppressor 10 in accordancewith an embodiment of the present invention. FIG. 2 is a perspective endview from the proximal end of flash suppressor 10 in accordance with anembodiment of the present invention. As shown, flash suppressor 10includes a central axis 12, a proximal end 14, and a distal end 16. Asused in this detailed description, the term “proximal” is used to referto the end of the component or element closest to the barrel of thefirearm and the term “distal” is used to refer to the end of thecomponent or element farthest from the barrel of the firearm. Proximalend 14 of flash suppressor 10 includes a threaded interface 18, which isused to connect flash suppressor 10 to the muzzle of a firearm that isnot shown in FIGS. 1 and 2. Flash suppressor 10 includes an angularshoulder 20 and threaded interface 22, which can be used to help connectflash suppressor 10 to another firearm attachment such as a noisesuppressor. Flash suppressor 10 also includes three tines 24, 26, and28. When a projectile is fired from a firearm attached to flashsuppressor 10, the gases proceed through the barrel of the firearm intoflash suppressor 10 and are dispersed by tines 24, 26, and 28 asexplained in more detail below.

FIG. 3 is a perspective view of individual tine 24 of the flashsuppressor of FIG. 1. FIG. 4 is an exploded perspective view of theflash suppressor of FIG. 1. As shown in FIG. 3, tine 24 is formed in ahelical shape. In this embodiment, tine 24 is formed using a helical cutthat can be measured in such a way whereby if tine 24 were extended 8.8inches it would form a complete rotation around a tube with a 0.9 inchdiameter. In this particular embodiment, the helical cut of each tine isoriented in clockwise, or right-handed twist, when viewed from thedirection of the projectile path through flash suppressor 10, This isthe same orientation of the rifling in most firearms.

FIG. 4 further shows the embodiment of the flash suppressor of FIG. 1.Flash suppressor 10 has a base 30, which consists of the portion offlash suppressor 10 from the distal end 14 through the proximal end ofangular shoulder 20. Base 30 has a circular face 32 that contains bore34. When a firearm is attached to flash suppressor 10, the muzzle of thefirearm (not shown) attaches to threaded interface 18 as shown in FIG.2. The bore of the barrel of the firearm aligns with bore 34. In thisembodiment, the diameter of bore 34 is the approximate size of thediameter of the bore in the barrel of the firearm. As also shown in FIG.4, tine 24 contains groove 36, tine 26 contains groove 38, and tine 28contains groove 39 wherein each groove is formed by making a cut of acertain width and depth from the distal end of the suppressor. Eachgroove reduces the weight of each tine, which improves the overallperformance of flash suppressor 10.

As the gases created from the firing of a projectile exit the barrel,these expelled gases proceed through bore 34 and are dispersed by tines24, 26, and 28 shown in FIG. 4. Each tine has an inner surface thatreceives the expelled gases through bore 34 and disperses the gases intothe ambient air to dramatically reduce, if not completely eliminate,muzzle flash by rapidly cooling and diluting the propellant gases asthey exit the firearm barrel. More specifically, tine 24 contains innersurface 40 and directs expelled gases in the direction shown by arrow42, which allows a portion of the expelled gases to be dispersed andmixed with ambient air through the cut between tine 24 and tine 28.Similarly, tine 26 contains inner surface 44 and directs expelled gasesin the direction shown by arrow 46, which allows a portion of theexpelled gases to be dispersed and mixed with ambient air through thecut between tine 24 and tine 26. Finally, tine 28 also contains an innersurface, which is not directly shown but indicated by arrow 48. Innerface 48 of tine 28 directs expelled gases in the direction shown byarrow 50, which allows a portion of the expelled gases to be dispersedand mixed with ambient air through the cut between tine 26 and tine 28.

FIG. 5 depicts the distal end view of flash suppressor 10 and, in thisparticular embodiment, inner surfaces 40, 44, and 48 of tines 24, 26,and 28, respectively, form a bore that has substantially the samediameter as bore 34. This particular spacing of tines 24, 26, and 28helps to ensure that the expelled gases are dispersed radially from thesuppressor through the cuts between the tines. This increases the ratein which the expelled gases are mixed with the ambient air and reducesthe chances of the gases igniting unused propellant before they areexpelled from flash suppressor 10.

In addition to significantly reducing, if not completely eliminatingmuzzle flash, flash suppressor 10 also eliminates any ringing caused bythe resonance of the tines. As shown in FIG. 6, in particularembodiments, cut 52 between tines 24 and 28 has a length 54 that islonger than cut 56 between tines 24 and 26 that has a length 58. Cut 60,which is shown in FIG. 7, has a length 62 between tines 26 and 28 and islocated on the back side of flash suppressor 10 in FIG. 6. In addition,the width of the cuts between tines 24, 26, and 28 can also be varied.As shown in FIG. 6, width 64 is between tines 24 and 28 and width 66 isbetween tines 24 and 26. Width 68 between tines 26 and 28 is shown inFIG. 7 and is located on the back side of flash suppressor 10 in FIG. 6.By varying the length and width of the individual cuts, the potentialfrequency of the individual tines can be varied to eliminate any audibleringing. In a particular embodiment of flash suppressor 10, which isdesigned to be used with a 0.223 caliber firearm, the length and widthof cuts 52, 56, and 60 that form tines 24, 26, and 28 are as follows:

Length 54 1.10 inches Width 64 0.3100 inches Length 58 1.05 inches Width66 0.3214 inches Length 62 1.00 inches Width 68 0.3275 inchesWith these particular dimensions, tines 24, 26, and 28 did not createany audible ringing when used with a firearm. While not shown in thisparticular embodiment, the frequency of tines 24, 26, and 28 canalternatively be varied to prevent an audible ringing by altering thedimensions of each groove 36, 38, and 39 in tines 24, 26, and 28,respectively, as shown in FIG. 4. In this particular embodiment, thecuts 52, 56, and 60 that form tines 24, 26, and 28 each rotate at least30 degrees around the central axis 12 (as shown in FIGS. 1 and 2) fromthe start of each cut to the finish of each cut.

In addition, as shown in FIGS. 6 and 7, in certain embodiments, tines24, 26, and 28 all extend to plane 70, which is perpendicular to thedistal end of the flash suppressor. When viewed from the distal end,surfaces 78, 80 and 82 shown in FIG. 5 all contact plane 70. Inaddition, as shown is FIG. 6, outer surfaces 72, 74, and 76 of the tines24, 26, and 28, respectively, are non-tapered. In other words, the outersurface of each tine remains an equal distance from the center of flashsuppressor 10 such that the outer diameter of the suppressor is samethroughout the length of tines 24, 26, and 28. Extending tines 24, 26,and 28 to the same plane, and keeping the outer diameter of thesuppressor the same throughout the length of the tines, helps ensurethat flash suppressor 10 is significantly easier to attach to otherfirearm components such as a noise suppressor. In addition, tines 24,26, and 28 are much less susceptible to being entangled in debris andother impediments during field use and uniformly absorb the impact if,for example, the firearm, to which flash suppressor 10 is connected, isdropped on its barrel.

By varying the length and widths of the cuts 52, 56, and 60, the mass ofeach of the tines is the same, which ensures that the flash suppressoris balanced for better performance.

While various embodiments of apparatus are described with—orwithout—certain features for ease of description and to illustrateexemplary aspects of those embodiments, the various components and/orfeatures described herein with respect to a particular embodiment can besubstituted, added, and/or subtracted from among other describedembodiments, unless the context dictates otherwise. Consequently,although several exemplary embodiments are described above, it will beappreciated that the invention is intended to cover all modificationsand equivalents within the scope of the following claims.

What is claimed is:
 1. A suppressor for a firearm, the suppressorcomprising: a proximal end; a distal end; and a plurality of tineswherein each tine is formed by a plurality of cuts in the distal end ofthe suppressor, each cut compromises a length and a width that differfrom each adjacent cut, and each tine has the same mass as each othertine.
 2. The suppressor of claim 1, wherein the length and width of eachcut vary such that each tine has the same mass as each other tine. 3.The suppressor of claim 2, wherein each tine extends to a planeperpendicular to the distal end of the suppressor.
 4. The suppressor ofclaim 3, wherein the length of each cut is at least one inch and thewidth of each cut is at least 0.3 inch.
 5. The suppressor of claim 3,wherein the length of each cut varies by at least three percent from thelength of each other cut, and wherein the width of each cut varies by atleast one and one half percent from the width of each other cut.
 6. Thesuppressor of claim 1, wherein each tine further comprises a non-taperedouter surface and a groove formed in the non-tapered outer surfacewherein the groove of each tine is formed such that each tine has thesame mass as each other tine.
 7. The suppressor of claim 1, wherein thesuppressor further comprises: a central axis through the center of thesuppressor from the proximal end to the distal end; a first interface atthe proximal end of the suppressor adapted to be coupled to a muzzle ofa firearm; a face adjacent to the first interface; a first bore with adiameter in the face; wherein each tine is a helical tine and eachhelical tine further comprises: an inner surface wherein the innersurfaces of the plurality of helical tines form a second bore with adiameter substantially the same as the diameter of the first bore; and anon-tapered outer surface.
 8. The suppressor of claim 7, wherein eachhelical tine rotates at least 30 degrees around the central axis.
 9. Thesuppressor of claim 7, wherein each helical tine further comprises agroove formed in the non-tapered outer surface wherein the groove ofeach tine is formed such that each helical tine has the same mass aseach other helical tine.
 10. A suppressor for a firearm, the suppressorcomprising: a proximal end; a distal end; a central axis through thecenter of the suppressor from the proximal end to the distal end; afirst interface at the proximal end of the suppressor adapted to becoupled to a muzzle of a firearm; a face adjacent to the firstinterface; a first bore with a diameter in the face; a plurality ofhelical tines wherein each helical tine further comprises: an innersurface wherein the inner surfaces of the plurality of helical tinesform a second bore with a diameter substantially the same as thediameter of the first bore; a non-tapered outer surface; and whereineach helical tine rotates at least 30 degrees around the central axis.